In many structural members the axial load and bending moment act simultaneously, producing a combined stress state that must be evaluated to ensure safety.
The linear superposition of axial and flexural stresses is expressed by the interaction equation
P = axial force (kN)
A = crossβsectional area (cmΒ²)
M = bending moment (kNΒ·m)
S = section modulus (cmΒ³)
The calculated stress is compared with the material yield stress, Fy, and the utilization ratio Ο/Fy is used to assess whether the member satisfies the design criteria.
What is the formula for combined axial bending stress?
How do I calculate the section modulus, S?
Why do we use linear superposition in this calculation?
What is the significance of comparing calculated stress with material yield stress?
Can this calculator handle different units of measurement?
What types of structural members can this calculation be applied to?
How do I interpret the results from this calculator?
Results are for informational purposes only and do not constitute professional advice.
